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WO2018196041A1 - Aérovélo - Google Patents

Aérovélo Download PDF

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Publication number
WO2018196041A1
WO2018196041A1 PCT/CN2017/083963 CN2017083963W WO2018196041A1 WO 2018196041 A1 WO2018196041 A1 WO 2018196041A1 CN 2017083963 W CN2017083963 W CN 2017083963W WO 2018196041 A1 WO2018196041 A1 WO 2018196041A1
Authority
WO
WIPO (PCT)
Prior art keywords
rotor
seat
frame
engine
gearbox
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/CN2017/083963
Other languages
English (en)
Chinese (zh)
Inventor
陶亮
申守建
李文明
陈登科
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Sun Hawk(henan) Aviation Industry Co Ltd
Original Assignee
Sun Hawk(henan) Aviation Industry Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Sun Hawk(henan) Aviation Industry Co Ltd filed Critical Sun Hawk(henan) Aviation Industry Co Ltd
Publication of WO2018196041A1 publication Critical patent/WO2018196041A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
    • B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
    • B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft

Definitions

  • the invention relates to the technical field of motorcycles, in particular to a flying motorcycle.
  • the object of the present invention is to provide a flying motorcycle, which solves the problem of the control of the flying motorcycle and the problem of the voyage, and makes the flying motorcycle truly reach the practical level, which is a leap-forward development of the history of the human aircraft.
  • a flying motorcycle comprising a frame and an engine mounted in the middle of the rack; the top and the bottom of the rack are respectively provided with a seat and a landing gear, and the seat passes through the seat
  • the chair damper is fixedly connected to the frame; the back of the seat is equipped with a catapult rescue umbrella, and the two sides of the seat are respectively equipped with a pitch roll joystick and a throttle stick; the position of the foot under the seat a heading bar is provided;
  • a gear box is mounted on both ends of the frame, and a retainer bracket is mounted on the top of the gear box, and a top of the retainer bracket is fixedly connected with the rotor retainer;
  • the gear box is internally mounted a pair of helical bevel teeth, and a transverse input shaft inside the gearbox is coupled to one end of the drive shaft through a coupling; the other end of the drive shaft is coupled to a power take-off shaft of the engine via a coupling; the pair of spiral
  • the lower part of the seat is equipped with a servo electronic flight controller, and the electronic flight controller of the steering gear is electrically connected to the rudder, and the three-axis gyro is mounted on the electronic flight controller of the steering gear. instrument.
  • an engine damper is installed between the engine and the frame.
  • the number of pieces of the rotor blade is 2-6 pieces, and the rotor pieces are evenly mounted on the rotor head.
  • the utility model has the beneficial effects that: the flying motorcycle of the invention, the power unit is powered by an aero-engine, and the transmission shaft axial direction front and rear two gear boxes are simultaneously outputted through a reduction gear box (the power can also be passed).
  • the engine crankshaft is directly output to the gearbox by the transmission shaft.
  • the gearbox is composed of a pair of spiral bevel gears.
  • the function of the gearbox is to change the power output direction from the front-rear direction to the upward output, and also has the function of the reduction gear box.
  • the output shaft of the box is mounted with a variable pitch rotor.
  • the number of rotors may be more than two pieces according to design requirements, generally no more than six pieces, and the upward lifting force is provided by the rotation of the two sets of front and rear rotors to fly the flying motorcycle off the ground;
  • the flying motorcycle has solved the problem of control of the flying motorcycle and the problem of navigation time, so that the flying motorcycle can truly reach the practical level, which is a leap-forward development of the history of human aircraft.
  • Figure 1 is a schematic view of the overall structure of the present invention
  • Figure 2 is a plan view of the present invention
  • Figure 3 is a schematic structural view of a gear box of the present invention.
  • a flying motorcycle comprising a frame 1 and an engine 2 mounted in the middle of the frame 1.
  • the frame 1 is made of metal pipe welding, and may also be lighter.
  • the material is made of a composite material such as carbon fiber;
  • the top and bottom of the frame 1 are respectively provided with a seat 3 and a landing gear 4, and the seat 3 is fixedly connected to the frame 1 through the seat damper 5;
  • the back of the 3 is mounted with a catapult 6 and the two sides of the seat 3 are respectively mounted with a pitch roll lever 7 and a throttle lever 8; a position of the foot below the seat 3 is provided with a heading pedal 9;
  • a gearbox 10 is mounted on both ends of the frame 1, and a retainer bracket 11 is mounted on the top of the gearbox 10, and a top of the retainer bracket 11 is fixedly coupled to the rotor retainer 12;
  • the gearbox 10 is internally mounted There is a pair of spiral bevel teeth 13, and the transverse input shaft 14 inside the gearbox 10 is connected to one end of the
  • the disk 20, and the first inclined rotor 21 at the upper portion of the swash plate 20 is fixedly coupled to the rotor blade 19 via the first link 22; the second inclined rotor 23 at the lower portion of the swash plate 20 is fixed to the steering gear 25 via the second link 24.
  • a lower portion of the seat 3 is mounted with a steering electronic flight controller 26, and the steering electronic flight controller 26 is electrically connected to the steering gear 25, and a three-axis gyroscope is mounted on the steering electronic flight controller 26;
  • An engine damper 27 is mounted between the frame 1 and the rotor blade 19 is mounted in a number of 2-6 pieces, and the rotor blades 19 are evenly mounted on the rotor head 18 at equal intervals.
  • the flying motorcycle of the invention adopts the combination of the control principle of the helicopter rotor and the flight control of the drone gyroscope, and the specific practices are as follows:
  • the rotor blade 19 of 18 is determined by the spacing of the blades, and a swash plate 20 for controlling the pitch is disposed under each set of the rotor mounting shafts.
  • the first inclined rotor 21 at the upper portion of the swash plate 20 passes through the first link 22 and each piece.
  • the rotor blades 19 are connected. When the swash plate 20 slides up and down, the rotor blade 19 of the rotor head 18 is correspondingly enlarged or smaller.
  • the swash plate 20 is composed of a first inclined rotor 21 and a second inclined rotor 23,
  • the intermediate shaft is connected by a bearing, the first inclined rotor 21 rotates with the rotor head 18, and the second inclined rotor 23 is connected to three steering gears 25 distributed at an angle of 120 degrees.
  • the steering gear 25 is an actuator for controlling the flight attitude, and is controlled by electronic flight.
  • the electronic flight controller 26 is designed with a three-axis gyroscope and an accelerometer, and other arithmetic circuits for controlling the attitude balance of the flying motorcycle.
  • the electronic flight controller 26 receives the pilot's joystick command. And control the steering gear to perform the action.
  • the second tilting rotor 23 does not rotate with the rotor, but the tilting angle can be sent by the pilot to the electronic flight controller 26 via the joystick, and the electronic flight controller 26 controls the second tilting rotor 23 through the steering gear 25 to control the tilt angle of the rotor surface.
  • the second inclined rotor 23 can be low or high, and can be left low and right high, or deflected in any direction, which allows the rotor surface to tilt in any direction, which changes the angle of the rotor during each rotation cycle.
  • the line controller 26 can achieve the purpose of complete synchronous control of the two sets of rotors before and after, but the two sets of front and rear rotors can only control the flight before and after the flight, and can not carry out the heading control. To achieve the heading control, it is necessary to control the airfoil of the front and rear rotors simultaneously. The two sides are inclined in opposite directions. In order to quickly and conveniently grasp the flying skills of the flying motorcycle, the heading control design is controlled by the heading mast 9, so that the whole flying motorcycle is handled in a similar manner to the traditional helicopter, making learning and driving easier.
  • the invention uses the electronic flight controller 26 to participate in the control of the flight attitude.
  • the electronic flight controller 26 is internally equipped with a three-axis gyroscope, the stability of the flight motorcycle is controlled by a three-axis gyroscope, which makes driving very simple and does not require precise With the skill and skill, the driver only needs to give the altitude and heading instructions.

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Toys (AREA)
  • Catching Or Destruction (AREA)

Abstract

La présente invention concerne un aérovélo. L'aérovélo comprend un cadre (1) et un moteur (2) monté au milieu du cadre (1), un siège (3) et un train de roulement (4) sont respectivement disposés en haut et en bas du cadre (1), et le siège (3) est relié de manière fixe au cadre (1) par l'intermédiaire d'un amortisseur de siège (5); un parachute d'éjection (6) est monté à l'arrière du siège (3), et une manette et un levier d'étranglement sont montés respectivement sur les deux côtés du siège (3); une tige de pédale de commande de cap (9) est disposé au-dessous du siège (3) où se trouve une pédale; des transmissions (10) sont montées aux deux extrémités du cadre (1), et un support de retenue (11) est monté au sommet de la transmission (10), et la partie supérieure du support de retenue (11) est relié de manière fixe à un élément de retenue de rotor (12); et une paire d'engrenages coniques en spirale sont montés à l'intérieur de la transmission (10), et un arbre d'entrée latéral à l'intérieur de la transmission (10) est relié à une extrémité d'un arbre d'entraînement par l'intermédiaire d'un couplage. L'aérovélo selon la présente invention résout les problèmes de commande et d'endurance des aérovélos.
PCT/CN2017/083963 2017-04-26 2017-05-11 Aérovélo Ceased WO2018196041A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CN201710283348.X 2017-04-26
CN201710283348.XA CN106904055A (zh) 2017-04-26 2017-04-26 一种飞行摩托

Publications (1)

Publication Number Publication Date
WO2018196041A1 true WO2018196041A1 (fr) 2018-11-01

Family

ID=59211240

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/CN2017/083963 Ceased WO2018196041A1 (fr) 2017-04-26 2017-05-11 Aérovélo

Country Status (2)

Country Link
CN (1) CN106904055A (fr)
WO (1) WO2018196041A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12221210B2 (en) 2021-10-25 2025-02-11 Levanta Tech Inc. Wing-in-ground effect vehicles and uses thereof

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108639320A (zh) * 2018-06-05 2018-10-12 河南三和航空工业有限公司 一种双旋翼无人直升机
CN113752765A (zh) * 2021-09-17 2021-12-07 熊辉 一种水陆空摩托车

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060208133A1 (en) * 2005-03-18 2006-09-21 Ligo Kenneth A Personal aircraft vehicle
CN101885295A (zh) * 2010-07-19 2010-11-17 杨朝习 陆空两用飞行器
CN104773290A (zh) * 2015-03-19 2015-07-15 南京航空航天大学 双涵道共轴多旋翼飞行摩托
CN204688413U (zh) * 2015-05-01 2015-10-07 张绍臣 直升机倾斜盘左右不对称球头夹
CN205468356U (zh) * 2016-04-05 2016-08-17 江苏数字鹰科技发展有限公司 一种具有座舱稳定系统的多旋翼飞行汽车或飞行摩托
WO2016142555A1 (fr) * 2015-03-12 2016-09-15 Martinez Gil Francisco Motocycle volant

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN204623828U (zh) * 2015-03-19 2015-09-09 南京航空航天大学 双涵道共轴多旋翼飞行摩托
CN205221109U (zh) * 2015-08-21 2016-05-11 河南三和航空工业有限公司 多轴载人飞行器
CN206664180U (zh) * 2017-04-26 2017-11-24 河南三和航空工业有限公司 一种飞行摩托

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060208133A1 (en) * 2005-03-18 2006-09-21 Ligo Kenneth A Personal aircraft vehicle
CN101885295A (zh) * 2010-07-19 2010-11-17 杨朝习 陆空两用飞行器
WO2016142555A1 (fr) * 2015-03-12 2016-09-15 Martinez Gil Francisco Motocycle volant
CN104773290A (zh) * 2015-03-19 2015-07-15 南京航空航天大学 双涵道共轴多旋翼飞行摩托
CN204688413U (zh) * 2015-05-01 2015-10-07 张绍臣 直升机倾斜盘左右不对称球头夹
CN205468356U (zh) * 2016-04-05 2016-08-17 江苏数字鹰科技发展有限公司 一种具有座舱稳定系统的多旋翼飞行汽车或飞行摩托

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12221210B2 (en) 2021-10-25 2025-02-11 Levanta Tech Inc. Wing-in-ground effect vehicles and uses thereof

Also Published As

Publication number Publication date
CN106904055A (zh) 2017-06-30

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